[fltsim.0]
title=Boeing 737-200 Air Berlin USA
sim=B737-200
model=
panel=
sound=
texture=abe
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_type=Boeing
atc_id_enable=1
atc_id=N2941
atc_id_color=0xffffffff
visual_damage=1
ui_manufacturer=Boeing
ui_type=737-200
ui_variation=Air Berlin USA
description=Boeing 737-200 Air Berlin USA, registration N2941W, repaint by Alf Werner 06.03, model by FFX\/SGA

atc_airline=AIR BERLIN
atc_heavy=0
atc_flight_number=

[forcefeedback]
gear_bump_nose_magnitude=3000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=2700		; 0 - 10000
gear_bump_left_direction=35500		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=00500		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=1300		; 0 - 10000
ground_bumps_angle1=08900		; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200		; 0 - 10000
ground_bumps_angle2=09100		; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000			; 0 - 10000
crash_direction1=01000			; 0 - 35999 degrees
crash_magnitude2=10000			; 0 - 10000
crash_direction2=9000			; 0 - 35999 degrees
crash_period2=75000			; in microseconds
crash_duration2=2500000			; in microseconds

[ground_reaction]
main_gear_static_compression=1.0		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.8            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.9		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.9		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[pitot_static]
vertical_speed_time_constant=1		//Increasing this value will cause a more instantaneous reaction in the VSI

[General]
performance=Model by Jorge Oppenheimer. \nEngine's type: P & W JT8D-9A \nWing span: 93 ft\nTotal height 37 ft. \nStatic T\/O Thrust (per engine) 14500 lb. \nMax. range 2600 km \nMax. T\/O weight 117000 lb. \nCruising altitude 31 - 35000 ft. \nMax. fuel weight 34592 lb. \nCruising speed 490 m.p.h. \nMax. payload structural 30200 lb.\nCargo capacity 875 cu. ft. \nOverall length 100 ft. 2 in. \nNumber of seats 117\n
atc_type=BOEING AIRCRAFT
atc_model=B732

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000, 0.000, 0.000, 0.000
empty_weight= 85000.000
empty_weight_roll_MOI= 1062809.000
empty_weight_pitch_MOI= 1411739.000
empty_weight_yaw_MOI= 1779732.000
empty_weight_coupled_MOI= 1300.000
max_gross_weight= 103759.999
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
Center1= 7.546, 0.000, 0.000, 2313.000, 0.000
LeftMain= 4.546, -19.000, 0.000, 1499.000, 0.000
RightMain= 4.546, 19.000, 0.000, 1499.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 980.000
wing_span= 93.000
wing_root_chord= 10.500
wing_dihedral= 5.999
wing_incidence= 0.000
wing_twist= -0.994
oswald_efficiency_factor= 4.997
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 408.000
htail_span= 41.667
htail_pos_lon= -37.167
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 305.000
vtail_span= 19.912
vtail_sweep= 0.000
vtail_pos_lon= -37.167
vtail_pos_vert= 5.833
elevator_area= 102.000
aileron_area= 39.200
rudder_area= 51.850
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 9.969
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 32.917, 0.000, -8.300, 1181.102, 0.000, 1.219, 53.700, 0.800, 2.500, 0.900, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -4.250, -8.580, -9.850, 1574.803, 1.000, 1.219, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -4.250, 8.580, -9.850, 1574.803, 2.000, 1.219, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 3.000, 0.000, 0.000

point.3= 2.000, -15.000, -46.500, 2.250, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -15.000, 46.500, 2.250, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -48.000, 0.000, 1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 34.833, 0.000, 1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 7.791




[GeneralEngineData]
engine_type= 1
Engine.0= 5.417, -15.833, -2.583
Engine.1= 5.417, 15.833, -2.583
fuel_flow_scalar= 1.000

[SMOKESYSTEM]
smoke.0=5.41,-2.58,-15.8, SMOKE_JT8D
smoke.1=5.41,-2.58,15.8, SMOKE_JT8D

[TurbineEngineData]
fuel_flow_gain= 0.004
inlet_area= 19.600
rated_N2_rpm= 29920.000
static_thrust= 15900.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 142.000
full_flaps_stall_speed= 113.600
cruise_speed= 395.375

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=35.832923,0.000000,4.588050

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0

[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.12,0.11  

[EFFECTS] 
wake=fx_wakewater=fx_spraydirt=fx_tchdr5concrete=fx_sparkstouchdown=fx_tchdwn, 1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 30.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.000
extending-time= 6.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000